Side-by-side
Flammability & Durability Testing (Airbus-Approved Lab) vs ZIM Crew Rest Module
Spec comparison for two products on Aviation Souk. Both compete in Aircraft Interior Fit-Out.
Aircraft Interior Fit-Out
Flammability & Durability Testing (Airbus-Approved Lab)
by Lantal Textiles AG
ISO/IEC 17025-accredited, Nadcap-certified flammability and durability testing laboratory in Langenthal, open to third-party aviation interior suppliers.
Aircraft Interior Fit-Out
ZIM Crew Rest Module
by ZIM Aircraft Seating GmbH
A removable lower-deck crew rest module that fits into the aircraft cargo bay to provide certified rest facilities for cabin or flight crew on ultra-long-haul operations.
| Cost of ownership | Flammability & Durability Testing (Airbus-Approved Lab) | ZIM Crew Rest Module |
|---|---|---|
| Price tier | — | — |
| Lead time (weeks) | ?–? | ?–? |
| Delivery | — | — |
| Install | — | — |
| GCC airports deployed | 0 | 0 |
| Certifications | 0 | 0 |
Specs
Technical specifications.
| Spec | Flammability & Durability Testing (Airbus-Approved Lab) | ZIM Crew Rest Module |
|---|---|---|
| Accreditation | ISO/IEC 17025 | — |
| Nadcap scope | Non-Metallic Materials Testing — Flammability (awarded Dec 2021) | — |
| Regulatory approval | EASA Production Organisation Approval (POA) | — |
| Certificate issued | EASA-recognised test certificate | — |
| Flammability standards covered | FAR/CS 25.853 (vertical + horizontal Bunsen burner, OSU heat release) | — |
| OEM smoke/toxicity standards | ABD 0031 (Airbus), BSS 7238 (Boeing) | — |
| Middle East lab location | Etihad Engineering facility, Abu Dhabi International Airport | — |
| Third-party testing | Available (airlines, OEMs, MROs, DOs) | — |
| Installation location | — | Lower-deck cargo compartment (removable) |
| Occupancy type | — | In-flight rest berths (not occupied during taxi, T/O, or landing) |
| Regulatory compliance basis | — | FAR Part 25 / CS-25 special conditions (fire, egress, smoke detection, O2) |
| Design approval | — | EASA Part-21J (ZIM design organisation EASA.21J.449) |
| Removal | — | Removable to restore full cargo capacity when not required |
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